JASC 2613
Service difficulty reports · 1,796
Reports filed under 2613 · Overheat Detection, newest first.
Query with SQL
duckdb -csv -c "SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE jasc_code = '2613' ORDER BY difficulty_date DESC"
Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.
SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE jasc_code = '2613' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR MASA200500417Clamp · looseASH 7130 IAD - RT 14TH STAGE DUCT WARNING IN FLIGHT. MAINTENANCE REPLACED LOOP AND SECURED LOOSE CLAMP.SDR AWXA200500615Warning Light · illuminatedON TAKEOFF ROLL AT LAS EN ROUTE TO SJC AT APPROXIMATELY 80-100 KTS. PILOT REPORTED AN ENGINE OVERTEMP. MX COMPLIED WITH POWER ASSURANCE TEST IAW AWA TASK CARD F5M71003 AND POWER ASSURANCE CHECK TEST 5 AND TROUBLESHOOTING CHART 71-00-42-1 STEPS 1, 2, 3 AND 25SDR 05062005Warning Light · illuminatedRT TAILPIPE HOT LIGHT ILLUMINATED DURING TAKEOFF ROLL.SDR MALA050402Sensor · dirtyON TAKEOFF ROLL, THE RIGHT TAIL PIPE HOT LIGHT ILLUMINATED. CREW ABORTED TAKEOFF AT 70 KNTS WITH MINIMUM BRAKING. CLEANED SENSOR.SDR MALA050403Sensor · dirtyIN MEM, THE CREW ABORTED THE TAKEOFF DUE TO HIGH TAIL PIPE TEMPERATURE INDICATION. CLEANED SENSOR.SDR 04242005Warning Light · illuminatedRT TAILPIPE HOT LIGHT ILLUMINATED.SDR RAIA00504024Overheat Loop · faultyFLT 5502 - CID - RT OVERHEAT WARNING. MAINTENANCE REMOVED AND REPLACED RT OVERHEAT LOOP ASSY.SDR DL76L050213Overheat Loop · failedCLIMBING THRU 10,000 FT, 10 MIN AFTER T/O RT DUCT LEAK EICAS AND RT DUCT LEAK ON OVERHEAD. REPLACED RIGHT DUCT OVERHEAT LOOP.SDR MALA050343Weu · malfunctionedRT TAIL PIPE HOT LIGHT. ABORTED FLIGHT. REMOVED AND REPLACED WEU.SDR 04022005Warning Light · illuminatedRT ENGINE TAILPIPE HOT LIGHT ILLUMINATED.SDR AMTA200500316Overheat Sensor · malfunctionedAFTER GEAR RETRACTION, WHEEL WELL FIRE LIGHT ILLUMINATED WITH FIRE BELL. COMPLETED WHEEL WELL FIRE PROCEDURES, LIGHT WENT OUT ON SHORT FINAL, BRAKE TEMPS WERE (0) DEG AND HYD NORMAL. REMOVED AND REPLACED OVERHEAT DETECTION CONTROL UNIT IAW MM. OPS CHECK GOSDR COMA0560205Sensor · faultyFLIGHT 5184 RECEIVED A RT 14TH STAGE DUCT MESSAGE DURING CLIMB OUT OF CVG. AIRCRAFT RETURNED TO THE FIELD. REPLACED THE 14TH STAGE HEAT SENSING ELEMENT.SDR COMA0560203Sensor · malfunctionedFLIGHT 5443 ABORTED TAKEOFF AT 10 KTS DUE TO LEFT JET OVERHEAT CAUTION, AIRCRAFT RETURNED TO THE GATE. DEFERRED JET OVERHEAT CAUTION PER MEL 16-11-02.SDR 2005UALA00258Wire · damagedLANDED UNDER AMBER ALERT DUE TO NR 2 ENGINE OIL FILTER BYPASS LIGHT. DETECTED A BROKEN SHIELD WIRE AT OIL FILTER SWITCH CONNECTOR. RETURNED TO ORD DUE TO NR 2 ENGINE OVERHEATED AND SHUTDOWN. SUPPLEMENTAL DATA UPDATE CREW REPORTED NR 2 ENGINE OVERHEAT INDICASDR 2005UALA00257Overheat Loop · malfunctionedRETURNED TO ORD DUE TO NR 2 ENGINE OVERHEATED AND SHUTDOWN. CREW REPORTED NR 2 ENGINE OVERHEAT INDICATION AT CLIMB. CREW SHUT DOWN NR 2 ENGINE PER QRC. PERFORMED TROUBLESHOOTING OF THE OVERHEAT DETECTION SYSTEM. FOUND NR 2 ENGINE CORE DETECTOR M1122, LOOPSSDR AMTA200500287Overheat Loop · defectiveEICAS STATUS MSG: L ENG OH LP2 DISPLAYED. REMOVED AND REPLACED LT ENG LOOP 2 OVERHEAT DETECTOR. REF; AMM 26-11-01. SYSTEM OPS CHECKED OK. (K)SDR AMTA200500288Warning System · intermittentEICAS STATS MSG: L ENG OH LB2 DISPLAYED INTERMITTENT. PERFORMED BITE PROCEDURE IAW FIM 26-11-00. LT ENG FIRE DETECTION SYS OPS CHECKS NORMALLY. NO STATUS MSG. DISPLAYED. OK FOR SERVICE. (K)SDR ANCF200400041Overheat Sensor · dirtyAFTER TAKEOFF, TAIL COMP TEMP LIGHT CAME ON. ABNORMAL CHECK LIST WAS PERFORMED AFTER LT ENGINE WAS REDUCED, 1.5 MIN LATER THE LIGHT WENT OFF, LT PACK WAS SWITCHED TO OFF AND LT ENG POWER RESTRICTED. IAW AMM 36-20-02 PAGE 201, TAIL COMPARTMENT OVERHEAT SENSORSDR 2005UALA00245Overheat Loop · malfunctionedSHUT DOWN NR 2 ENG DUE TO OVERHEAT INDICATION. CREW REPORTED NR 2 ENG OVERHEAT LIGHT CAME ON WITH NO ABNORMAL ENGINE INDICATION. OVERHEAT LIGHT STAYED ON AFTER THE CHECKLIST. CREW SHUT DOWN NR 2 ENGINE. OVERHEAT LIGHT WENT OUT. UPON ARRIVAL AT THE GATE BOTHSDR 03082005Warning Light · illuminatedRT TAILPIPE HOT LIGHT ILLUMINATED.SDR GAIA05013AOPWarning Light · illuminatedFLT 750 - MIA - DURING CLIMB-OUT, THE LOWER AFT BODY OVERHEAT LIGHT CAME ON. THE AIRCRAFT RETURNED TO MIA AND AN UNEVENTFUL LANDING WAS MADE. (M)SDR AMT2005F00001Warning Light · illuminatedLT ENGINE OVERHEAT EICAS CAME ON AT CRUISE, ALT (40000) PERFORMED FIM 26-12-00, FIG 103, FOUND NO DEFECTS. RAN ENGINE TO HIGH POWER SETTING WITH NO DEFECTS. OPERATIONAL CHECK NORMAL. (GL11200507753) (K)SDR AMTA200500168Warning System · malfunctionedLT ENG OVHT EICAS CAME ON AT CRUISE ALT (40000) PERFORMED ENG OVHT CHECK LIST AND SHUTDOWN LT ENG. PERFORMED FIM 26-12-00, FIG 103 FOUND NO DEFECTS. RAN ENGINE TO HIGH POWER SETTING WITH NO DEFECTS. OPERATIONAL CHECK NORMAL. (K)SDR AMTA200500169Warning System · activatedSTATUS MSG R TURB OH DET 2 DISPLAYED. PERFORMED FIM 26-13-00, FIGS 103 AND 104 MSG.SDR RAIA00502018Sensor · defectiveSTL - BLEED LEAK INDICATION NR 1 ENGINE. MAINTENANCE REMOVED AND REPLACED BLEED LEAK SENSOR IN NR 1 PYLON.SDR AMTA200500152Warning System · activatedLT STRUT OH DET 1 DISPLAYED. NO ANOMALIES FOUND IAW FIM. OPS CHECK GOOD AT THIS TIME IAW AMM. (K)SDR 2005UALA00105Overheat Loop · damagedDIVERTED TO SFO DUE TO WING BODY OVERHEAT INDICATION. CREW REPORTED RIGHT WING BODY OVERHEAT LIGHT ILLUMINATED DURING CLIMB. PERFORMED TROUBLESHOOTING OF THE OVERHEAT DETECTION SYSTEM AND CONFIRMED A SHORT WITH RIGHT WING LEADING EDGE OVERHEAT DETECTOR LOOP MSDR 05636028Overheat Loop · malfunctionedEVENT SUMMARY STATED ENG SHUTDOWN DURING FLIGHT. REMOVED AND REPLACED LT 14TH STAGE OVERHEAT LOOP REF 26-12-00. OPS CHECK GOOD AT THIS TIME.SDR AMTA200500091Warning System · malfunctionedLT STRUT O/H DET 1 DISPLAYED. PERFORMED FIM 261200FIG103/104 NO FAULTS FOUND ALSO AFLOTS CARD INDICATIONS LED INDICATE NO FAILURES. (K)SDR C7WA200400072Warning Light · illuminatedLOWER AFT BODY OVERHEAT LIGHT ILLUMINATED THEN EXTINGUISHED ON ITS OWN INFLIGHT. INSPECTED DUCTING IN AFT AIRSTAIR AREA AND RAN ENGINES AT TAKEOFF POWER. UNABLE TO DUPLICATE PROBLEM, NO LEAKS NOTED. SYSTEM OPERATIONAL, CHECK GOOD IAW MM. (K)SDR C7WA200400073Sensing Element · erraticIN FLIGHT, LOWER AFT BODY OVERHEAT LIGHT ILLUMINATED, RT DUCT PRESSURE INDICATED 80 PSI. MADE PRECAUTIONARY LANDING. TIGHTENED ALL CLAMPS IN AIRSTAIR AREA. REPLACED LT AND RT PURGE LINE COUPLING SEALS. REMOVED AND REPLACED LOWER AFT BODY OVERHEAT LOOP DETESDR COMA0560037Overheat Loop · malfunctionedFLIGHT 9487 ANTI ICE DUCT WARNING. REPLACED THE RIGHT WHEEL WELL SENSING LOOP.SDR CX7A194J0506Detector · saturatedLT TAIL PIPE HOT ON TAKE OFF. ABORTED.SDR CX7A194J0505Detector · saturatedLEFT TAILPIPE HOT LIGHT ILLUMINATED ON TAKEOFF.SDR 2005UALA00026Sensing Element · damagedCREW REPORT NR 1 ENG -A- OVERHEAT LIGHT ILLUMINATED. *S/D* CREW REPORTED NR 1 ENGINE -A- LOOP OVERHEAT LIGHT ILLUMINATED. SHUTDOWN ENGINE AND DISCHARGED BOTH FIRE EXTINGUISHER BOTTLES. OVERHEAT DETECTION LOOP -B- WAS INOPERATIVE AND DEFERRED, ELIMINATING RSDR MALA050101Warning Light · illuminatedRIGHT TAIL PIPE HOT MASTER WARNING LIGHT CAME ON OUR INITIAL CLIMB, PERFORMED MEMORY ITEMS AND QRH CHECK LIST WARNING LIGHT WENT OUT. AIR RETURN TO MEM. MAINTENANCE RAN AC FOR 30 MINUTES COULD NOT DUPLICATE TAIL PIPE HOT LIGHT. OPS CHECK GOODSDR COMA0560019Overheat Sensor · faultyFLIGHT 5224 LEFT WING OVERHEAT MESSAGE WHEN DEICE SELECTED OFF. REPLACED THE OVERHEAT SENSOR.SDR AMTA200401493Warning System · malfunctionedLT ENG OH DET 1 LOOP STATUS MSG FOLLOWED BY LT ENG OVHT EICAS. WAS ABLE TO GET OVHT LIGHT TO EXTINGUISH AFTER COMPLETING QRH PROCEDURES NNC 7.21. PERFORMED FIM PROCEDURE 26-12-00, NO DEFECTS NOTED. (K)SDR CX7A194J0459Detector · contaminatedSHORTLY AFTER ROTATION GOT A LEFT HAND TAILPIPE HOT INDICATION.SDR MALA040772Sensor · contaminatedAFTER TAKEOFF THE RT TAIL PIPE HOT LIGHT ILLUMINATED. AIR RETURN TO MEM. MAINTENANCE APPLIED SEALENT TO TAIL PIPE SENSORS IAW SMM CHP 54-30-05-2 OPS CHECK GOOD IAW SMM CHP 26-11-00-5.SDR DHL200436310Indicator · inoperativeAPPROXIMATELY 15 MINUTES AFTER TAKEOFF AT FLIGHT LEVEL 290, THE BRAKE TEMP ON WHEEL NR 8 INDICATED 700 DEGREES AND BRAKES HOT ILLUMINATED ON MASTER WARNING PANEL. ABNORMAL PROCEDURE COMPLETED ON LANDING APR BRAKE. T/S, SUSPECT F/E NR 8 BRAKE TEMP INDICATION SDR 341014Warning Light · illuminatedRIGHT TAILPIPE HOT LIGHT ILLUMINATED.SDR 2004UALA01173Overheat Loop · failedDIVERTED TO SLC DUE TO WING BODY OVERHEAT INDICATION. DISCREPANCY FOUND TO BE NR 2 ENGINE, STRUT CAVITY OVERHEAT DETECTOR ELEMENT FAULT. REPLACED OVERHEAT DETECTOR SENSING ELEMENT OF NR 2 ENGINE STRUT CAVITY .SDR 04330649Overheat Loop · malfunctionedL 14TH STAGE DUCT WARNING. ENGINE AT IDLE. DIVERT TO NEAREST AIRPORT, LANDED SAFELY. MX REMOVED AND REPLACED DUCT LOOP.SDR 2004UALA01149Overheat Loop · failedDIVERTED TO PIT DUE TO WING BODY OVERHEAT INDICATION. DISCREPANCY FOUND TO BE NR 2 ENGINE, STRUT CAVITY OVERHEAT DETECTOR ELEMENT FAULT. REPLACED OVERHEAT DETECTOR SENSING ELEMENT OF NR 2 ENGINE STRUT CAVITY .SDR 2004UALA01041Overheat Loop · malfunctionedDIVERTED TO COS DUE TO WING BODY OVERHEAT INDICATION. EXPERIENCED RIGHT WING BODY OVERHEAT WARNING IN FLIGHT WITH ENGINE SUPPLYING AIR. ISOLATED TO RIGHT WING LEADING EDGE OVERHEAT DETECTOR LOOP M1204. REPLACED OVERHEAT DETECTOR LOOP M1204. SYSTEM OPERATIOSDR DHL2004760012Control Panel · malfunctionedOVERHEAT DETECTION SYSTEM STRUT AND LOWER AFT BODY LIGHTS ALL ILLUMINATED. WOULD NOT EXTINGUISH. FOUND TEST SWITCH FOR OVHT DETECTION SYSTEM FOR STRUTS AND LOWER AFT BODY LIGHTS INOP. DEFFERED TEST FUNCTION PER ASTAR MEL 26-10-2. CAT C CONTROL NR 18357. PSDR QXEA200400736Warning Light · false indicationYYC - FLIGHT 2335 - THE FLIGHT RETURNED TO FIELD AFTER THE CREW RECEIVED A FLIGHT COMPARTMENT AND CABIN DUCT HOT CAUTION LIGHTS. THE DUCT TEMPS WERE NORMAL. CABIN WOULD NOT PRESSURIZE AFTER CYCLING THE AUTO AND MANUAL BLEED SWITCHES. MAINTENANCE INSPECTED TSDR RAIA00410027Sensor · malfunctioned8052 - IAD - BRAKE TEMP NR 3 OVERHEAT INDICATION. MAINTENANCE DEFERRED NR 3 BRAKE TEMP SYSTEM AND SUBSEQUENTLY CLEARED THE DEFERRAL BY REMOVING AND REPLACING THE NR 3 TEMP SENSOR.SDR COMA0460572Control Unit · malfunctionedFLIGHT 5263 LT ENGINE JET OVERHEAT CAUTION MESSAGE. REPLACED THE FIRE/OVERHEAT CONTROL UNIT.
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